N978DL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,035 hrs · 54,492 cycles

FWD OVERWING EXIT EMERGENCY EXIT LIGHTS INOP AT ROW 24. REPL BATTERY PACK PER AMM 33-53. OPS CHECK GOOD. (LP5588474)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,580 hrs · 54,070 cycles

FWD OVERWING EMER EXIT SIGNS OUT ON WALK AROUND. R/R EMER LIGHT BATTERY PACK B5-103 REF AMM 33-53. ALL CKS NORMAL. (LP5846431)

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 72,334 hrs · 53,854 cycles

ON WAKEUP CK FOUND #2 ENG LARGE DENT APPOX 3" LONG AND .250" DEEP IN NOSE COWLING AT 4 O'CLOCK POS. REMOVED #2 ENG NOSE COWL PER AMM 71-10-01 INSTALLED #2 ENG NOSE COWL PER AMM 71-10-01. COWL, NOSE, LT OFF 88-7110-9-0001 02236 ON 88-7110-9-0001 49422. (LP6253752)

Part: DOUBLER — WORN (RT WING) · airframe 72,272 hrs · 53,800 cycles

AWR WORN ON PREVIOUS REPAIR DOUBLER STA XFLS 158 LEADING EDGE AT RT WING ON REFERENCE MON /097/023 LOG 2981072. DOUBLER WAS REPLACED PER ER/A 557670-14 REV. ORIGINAL SECTION I. (LP1075873)

Part: VANE — DAMAGED (TE FLAP) · airframe 72,272 hrs · 53,800 cycles

INITIAL INSPECTION; MISSING COMPOSITE MATERIAL AND PUNCTURE ON LOWER SKIN SURFACE ON MID FLAP GUIDE VANE AT OUTBD FLAP RT WING. OUTBD FLAP RT WING WAS REMOVED PER AMM 27-51-03-201 STEP 3 AND GUIDE VANE AT OUTBD FLAP PN: 5910042-512 S/N: DL120 RT WING WAS INSTALLED PER AMM 27-51-03 3B(1) TO 3B (12). VANE, CTR, OTBD OFF 92-2750-9-0003 20004 ON 09-2750-9-0008 00120. (LP1076381)

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 72,272 hrs · 53,800 cycles

REF CARD 2500-4425: DURING OPERATIONAL CHECK OF MEGAPHONE HARDWARE DAMAGED WAS FOUND. MEGAPHONE P/N: A3-06-1402-1 S/N: 3522 WAS REMOVED AND SERVICEABLE MEGAPHONE P/N: EM1D S/N: N/A WAS INSTALLED AND INSTALLATION TEST WAS PERFORMED PER AMM 23-34-00. INSTALLATION TEST OK. (LP1066990)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,098 hrs · 53,642 cycles

1ST EMERGENCY ESCAPE PATH LIGHT AFT OF AFT ENTRY DOOR DAMAGED INOP. REPL LIGHT ASSY PER AMM 33-53. OPS CHECK GOOD. (LP4882856)

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,964 hrs · 53,523 cycles

FOUND L & R FWD OVERWING EXIT LIGHTS INOP. FOUND BATTERY POWER SUPPLY UNIT FOR L & R OVERWING EXIT LIGHTS INOP. R+R BATTERY SUPPLY UNIT PER AMM 33-53. OPS CHECK GOOD. A/C OK FOR SVC. SN OFF 24552 SN ON 27370. (LP5826667)

Part: TRANSDUCER — FAULTY (NR 1 WHEEL) · airframe 71,964 hrs · 53,523 cycles

LT OUTBD ANTI-SKID MESSAGE ON FINAL AFTER GEAR EXTENSION. RAN QRH, STAYED ON. FOUND LT OUTBD ANTI-SKID HAS FAULT. R/R NR 1 WHEEL SPEED TRANSDUCER REF AMM 32-43. PERFORMED WHEEL SPIN UP CHECK PER AMM 32-43 + SHOOK DOWN WIRING ON GEAR- ALL OPS OK- FAULTS CLEARED. OK FOR SVC. SDR REPORTED DUE TO FACT THAT MCC INDICATED THAT AN EMERGENCY LANDING WAS DECLARED DURING THIS EVENT. (LP5826665)

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,925 hrs · 53,494 cycles

FWD OVERWAY EMER "EXIT INTERIOR LIGHTS LT & RT DO NOT ILLUM. R/R BATTERIES IN PACK FOR SAME. REF AMM 33-53. OPS CK GOOD. (LP5826648)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,886 hrs · 53,458 cycles

OVERWING-AFT EMERGENCY LIGHTS INOP. INSIDE THE CABIN. REPLACED BATTERIES IN POWER SUPPLY FOR LT AND RT AFT EMERGENCY ESCAPE HATCH EXIT LIGHTS. OPS CK GOOD. (LP5826626)

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,555 hrs · 53,199 cycles

GALLEY EMERG LIGHTS INOP. REPLACED BATTERIES. OPS CK GOOD REF AMM 33-53. (LP4648349)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 71,426 hrs · 53,100 cycles

LAVATORY SMOKE DETECTOR WILL NOT TURN OFF - LOCATIONS 203. SMOKE DETECTOR WILL NOT TURN OFF. R/R SMOKE DET/BATT ASSY. NOW OPS NORM. REF MD88 AMM 26-17. (LP0866578)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,114 hrs · 52,829 cycles

FWD RIGHT OVER WING EMERGENCY EXIT LIGHT INOP. RELAMPED IAW MD88 AMM 33-53-00. (LP4414997)

Part: WIRE — BROKEN (CATWALK) · airframe 69,974 hrs · 51,914 cycles

EMERG LIGHT ON CATWALK INOP DUE TO BROKEN WIRE. RETERMINATED WIRE PER SPWM CH 20 CKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,937 hrs · 51,882 cycles

AFT OVER WING HATCHES DOOR LT AND RT EXIT LIGHT INOP. R&R EMERGENCY LIGHT BATTERIES FROM BATTERY PACK B5-105. OPERATIONAL CHECK GOOD, IAW AMM 33-53.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,773 hrs · 51,753 cycles

FOUND BROKEN WIRES AT SEAT E 21, EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CONNECTOR IAW SWPM 20-1, OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,665 hrs · 51,659 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE ABOVE ROWS 23-26. REPLACED THE BATTERY PACK AT B5104 IAW AMM 33-53. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,133 hrs · 51,236 cycles

AFT EMERGENCY LIGHTS OVER LEFT AND RIGHT WINDOW INOP. REMOVED AND REPLACED 'D' CELL BATTERIES IN BATTERY CHARGER 5105. OPERATIONAL CHECK GOOD. P/N AD-4002P.

Part: SMOKE DETECTOR — MISSING (LAVATORY) · airframe 69,123 hrs · 51,228 cycles

FOUND RT AFT LAV MISSING SINGLE STATION SMOKE ALARM. REPLACED MISSING RT AFT LAV SMOKE DETECTOR IN REF WITH AMM 26-13. TESTS GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,873 hrs · 51,041 cycles

FOUND EXIT LIGHT IN ROW 25ABC & 25DE INOP. REPLACED BATTERY PACK POWER SUPPLY ASSY. OPS CKS GOOD PER MD88 AMM 33-53. (LP3817447)

Part: SPAR CAP — CRACKED (RT WING) · airframe 67,289 hrs · 49,766 cycles

RT WING REAR SPAR LOWER CAP AT STATION XRS=164.000 SHOWS SIGN OF CRACK INDICATION. COMPLIED WITH PRI'S 557104-14 REV 0, 1, 2, 3. REPAIRED REF ERA 557104-14 REV A.

Part: DOUBLER — NOT REPORTED (TE FLAP) · airframe 72,272 hrs · 53,800 cycles

ERA 557670-14 SECTION I ISSUED FOR REPAIR INSTALLED ONTO NOSE SKIN ON RT MAIN FLAP AT APPROX XFLS158. FOLLOW ON ACTION IS REQUIRED. DOUBLER REPAIR WAS REPLACED PER ER/A 557670-14 REV.ORIGINAL SEC. I NRC 00048 UNDER LP 1075873. PLEASE CLOSE THIS LOG 2981072. ITS A MAJOR REPAIR (LP2981072)

Part: FLOOR PANEL — CORRODED (BS 163) · corrosion level 2 · airframe 67,289 hrs · 49,766 cycles

EVIDENCE OF POSSIBLE CORROSION FWD GALLEY FLOOR. BS 163 AND RBL 7 COMPLIED WITH PRI 557511-14 REV 0, 1, AND 2. REPAIRED IAW ERA 557511-14, REV ORIG.

Part: SPAR — CRACKED (WING) · airframe 67,289 hrs · 49,766 cycles

WING REAR SPAR CRACKED AT XRS 164, A DOUBLER REPAIR WAS ACCOMPLISHED.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 67,089 hrs · 49,618 cycles

EMERGENCY LIGHT INOPERATIVE BY EMERGENCY SLIDE IN TAIL. RESEATED THE CONNECTOR, OPS CHECKED SATISFACTORY.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 67,089 hrs · 49,618 cycles

EMERGENCY LIGHT INOPERATIVE IN CEILING SECOND AFT OF AFT CABIN DOOR. RESEATED THE CONNECTOR. OPS CHECKED SATISFACTORY.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 67,089 hrs · 49,618 cycles

EMERGENCY LIGHT INOPERATIVE IN CEILING JUST AFT OF AFT CABIN DOOR. FOUND THE SOCKET DAMAGED. REPAIRED THE SOCKET. LIGHT OPS NORMAL. 6)

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 66,768 hrs · 49,373 cycles

RIGHT AND LEFT FWD OVERWING EXIT LIGHT EMERGENCY INOPERATIVE. FOUND HIGH RESISTANCE IN GROUND WIRE L1228B16N FOR BATTERY PACK B5-103. FOUND GROUND WIRE TERMINAL LUG FOR WIRE L1228B16N LOOSE, SECURED THE WIRE AND RESISTANCE NOW GOOD. INSTALLED WIRE TO BATTERY PACK TERMINAL WDM 33-51-11 AND 33-51-12 OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,574 hrs · 49,247 cycles

FORWARD EMERGENCY LIGHT AT THE L1 AND R1 DOORS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-55. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,560 hrs · 49,235 cycles

EMER CEILING LIGHTS FROM ROW 23 THRU 25 INOP. REPLACED EMER LIGHTS BATTERIES NO HELP. R&R BO B5104.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,560 hrs · 49,235 cycles

BOTH LEFT AND RIGHT FWD OVERWING UPPER EMER EXIT LIGHTS INOP. REPLACED EMER LIGHT BATTERIES, NO HELP. R&R BP B5103. CKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,192 hrs · 48,930 cycles

LEFT AND RIGHT FWD OVERWING EXIT LIGHTS INOPERATIVE DURING TEST. REPLACED THE BATTERY PACKS. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,793 hrs · 48,630 cycles

CEILING EMERGENCY LIGHTS AT ROWS 22-25 ARE INOPERATIVE. REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK, OPS CHECKS GOOD IAW MM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,793 hrs · 48,630 cycles

CEILING EMERGENCY LIGHTS AT ROWS 11-14 ARE INOPERATIVE . REMOVED AND INSTALLED NEW EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW MM 33-53-00.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 65,358 hrs · 48,296 cycles

L1 SLIDE BUSTLE FELL OUT. R & R L1 DOOR SLIDE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,711 hrs · 47,830 cycles

FOUND THE LT AND RT AFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK FOR THE EXIT LIGHTS. THE LIGHTS CHECKED OK.

Part: LANYARD — MISROUTED (TAILCONE) · airframe 64,573 hrs · 47,734 cycles

MAINTENANCE FOUND THE TAILCONE RELEASE LANYARD ROUTED INCORRECTLY. THE TAILCONE RELEASE LANYARD WAS PROPERLY ROUTED. A FUNCTIONAL CHECK OF THE RELEASE SYSTEM WAS CONDUCTED AND CHECKED.

Part: CUSP WEB — CORRODED (BS 864-886) · corrosion level 2 · airframe 62,843 hrs · 46,504 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 TO X=60 BETWEEN BS 864 - 886. CUSP WEB REPAIRED IAW SRM 51-10-3, PAR 14, 21, AND 53-05, FIG 131A-14.

Part: SKIN — DAMAGED (RT WING) · airframe 62,834 hrs · 46,497 cycles

DURING REMOVAL OF THE RT TDG NO FOD HEATER BLANKET, THE NR 10 FASTENER HOLE IAW TDG DWG 3093, LOCATED AT XCW=116.6 APPROXIMATELY ON THE T/E WAS FOUND EXCESSIVELY COUNTERSUNK AND ELONGATED THRU THE UPPER WING SKIN PN 5930502-118. AREA WAS REPAIRED IAW ER/A 534402-14AD, REV A.

Part: LONGERON SPLICE — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LONGERON SPLICE 25R BETWEEN BS 1136 AND 1155. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-10-4, 51-30-5, AND 51-10-3 PAR. 14, 21, AND 38.

Part: FRAME — CRACKED (BS 427) · airframe 62,823 hrs · 46,490 cycles

CRACK ON FRAME BS 427 BETWEEN LONGERONS 24 - 25R. DAMAGE WAS REMOVED IAW AND REPAIR FABRICATED, TREATED, PAINTED, AND INSTALLED IAW ER/A 534376-14 REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION WAS FOUND ON THE LT CARGO TRACK BS 1220 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-1, AND DWG 5936660

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON REPAIR SPLICE OF FRAME AT BS 1307 BETWEEN LONGERONS 29L TO 29R. REPAIRED THE FRAME IAW SRM 53-03 D FIG 2A.

Part: DOOR FRAME — CORRODED (BS 370-427) · corrosion level 2 · airframe 62,823 hrs · 46,490 cycles

SEVERE CORROSION ON OUTER SURFACE OF DOOR FRAME FROM BS 370-427 AND LONGERON 28R. DOOR FRAME SECTION WAS REMOVED AND NEW SECTION INSTALLED IAW SRM 53-05, FIG 44A.

Part: FRAME — CORRODED (BS 1322) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON FRAME BS 1322 LONGERON 29L. THE FRAME WAS REPAIRED IAW SRM 53-03D FIG 2.A SHEET 3.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LEFT WING ACCESS PANELS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — CRACKED (BS 1401-1429) · airframe 62,823 hrs · 46,490 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN AT BS FROM BS 1401 - 1429 BETWEEN LONGERONS 1 AND 3 RT. REPAIRED IAW ER/A 534369-14AD, REV ORIGINAL.

Part: INTERCOSTAL — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1136 AND 1155 AND LONGERON 29 AND 30R. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 1098-1112) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN BS 1098 - 1112 BETWEEN LONGERONS 27 - 29L. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-04 FIG 57, 51-10-3 P. 21-14, 51-30-5.

Part: FINGER DOUBLER — CORRODED (BS 588-617) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON FINGER DOUBLER FROM LONGERON 26L BTW BS 588-598, 607-617. FABRICATED, TREATED, AND PAINTED A NEW DOUBLER AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-04-3 FIG. 12 (SHEET 1) 51-10-3 PAR 14, 21.

Part: LONGERON — CRACKED (BS 1307) · airframe 62,823 hrs · 46,490 cycles

CRACK ON LONGERON 6L BS 1307. LONGERON REPLACED IAW SRM 53-02, FIG 18, SHT 1.

Part: LONGERON SPLICE — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LONGERON SPLICE END 25R BETWEEN BS 1212 AND 1231. LONGERON SPLICE WAS REPLACED DUE TO EXCESIVE CORROSION IAW DWG 5936007 REV AR AND SRM 51-30-05.

Part: INTERCOSTAL — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1136 AND 1155 LONGERON 29L. INTERCOSTAL WAS REPLACED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON COUNTERSINK AREA OF RT WING FUEL ACCESS PANEL 1436C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A

Part: LONGERON — CRACKED (BS 1437) · airframe 62,823 hrs · 46,490 cycles

CRACKED LONGERON 3L BS 1437 AFT ACCESSORIES COMPARTMENT. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: DOUBLER — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION REPAIR DOUBLER BS 1155 - 1174 RT SIDE BETWEEN X -54 TO X -60 IN THE PAX CABIN. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3 P. 21 AND 14, AND 53-05 FIG 131A.

Part: CUSP WEB — CORRODED (BS 1103-1132) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT CUSP WEB AT BS 1103 - 1132 BETWEEN X -54 TO X -60. CUSP WEB WAS REPAIRED, TREATED, AND PAINTED IAW SRM 53-05 FIG 131A-14, 51-10-3 PAR 14 AND 21, 51-30-1, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1196-1209) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT CUSP WEB BS 1196 - 1209, X -54 TO X -60 IN PAX CABIN. THE DAMAGE WAS REMOVED IAW SRM 53-05 FIG 131A-5. A REPAIR WAS FABRICATED IAW SRM 53-05 FIG 131A-5. THE REPAIR WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. THE REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1023-1095) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT CUSP WEB BS 1023 - 1095 BETWEEN X -54TO X -60 IN PAX CABIN. THE CUSP WEB WAS REMOVED, A NEW CUSP WEB WAS DRILLED, TREATED, INSTALLED IAW SRM 51-10-3, 51-30-2, 51-30-5, 51-30-1, 51-10-4, AND 51-10-3 PAR 21, 14, AND 38.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON COUNTERSINK AREA OF RT WING FUEL ACCESS PANEL 1414C. THE CORROSION WAS REMOVED AND THE ACCESS PANEL WAS FOUND TO BE OUT LIMITS AND REPAIRED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,823 hrs · 46,490 cycles

CRACKED LONGERON 2L BS 1418 AT AFT ACCESSORIES COMPARTMENT. THE LONGERON WAS REMOVED AND A NEW LONGERON WAS FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-02, FIG 18, 51-10-3 PARA 21, 14 51-30-5.

Part: CUSP WEB — CORRODED (BS 501-598) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT CUSP WEB BS 501 TO 598 BETWEEN X=-54 TO X -60 IN PAX CABIN. REMOVED THE CUSP WEB IAW SRM 51-30-1, 51-30-2, 51-30-5, DRILLED A NEW CUSP WEB IAW SRM 51-10-4 CUSP WEB WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR. 21 AND 14, AND INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT CUSP WEB BS 598 TO 712 BETWEEN X -54 TO X -60 IN PAX CABIN. THE CUSP WEB WAS REPLACED IAW SRM 51-30-5, 51-30-2.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON FLOOR PANEL 256A IN PAX CABIN. A NEW FLOOR PANEL WAS DRILLED, TREATED, AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21 AND 51-10-4.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON RT WING FUEL ACCESS PANEL 1472C. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON FLOOR PANEL 256E IN PAX CABIN. A NEW FLOOR PANEL WAS DRILLED AND TREATED IAW DC9/MD80 SRM 51-10-3 PAR. 14 AND 21 AND 51-10-4.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON COUNTERSINK AREA ON FUEL ACCESS PANEL 2302 ON THE CENTER FUEL TANK. THE CORROSION WAS REMOVED AND FOUND TO BE OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — DAMAGED (BS 197-200) · airframe 62,823 hrs · 46,490 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN BETWEEN STA Y=200 TO 197 AND BETWEEN LONG 16 TO 18 RT. STR-ENG, CARD 8, ZONE 46. THIS REPAIR WAS PERFORMED BY THE ER/A 473065-14AD.

Part: CUSP WEB — CORRODED (BS 601-616) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION OUT LIMITS ON LT CUSP WEB BETWEEN X 60 TO X 54 AT BS 601, AND FROM BS 609 TO 616. REPAIR WAS ACCOMPLISHED IAW SRM 53-05 FIG 131A-11, AND SRM 51-10-3 PAR. 14 AND 21.

Part: CUSP WEB — CORRODED (BS 757-779) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LT CUSP WEB X 60 - 54 BETWEEN BS 757 - 766, 778 - 779. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.

Part: LONGERON — CRACKED (BS 845) · airframe 62,823 hrs · 46,490 cycles

CRACKED LONGERON 5L BS 845. LONGERON WAS REMOVED, AND A NEW SECTION OF LONGERON WAS TRIMMED OUT AND DRILLED, NEW SECTION OF LONGERON WAS TREATED AND PAINTED, NEW SECTION OF LONGERON WAS INSTALLED, NEWS SPLICES WERE FABRICATED, ADJUSTED AND DRILLED, SPLICES WERE INSTALLED IAW AMM 20-10-11. SRM 51-30-2, 53-02, FIG 18, 51-10-3, 51-30-5.

Part: CUSP WEB — CORRODED (BS 474-475) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LT CUSP WEB FROM BS 474 TO 475 BTW X 56 AND X 60. DAMAGE WAS REMOVED IAW SRM 53-05 FIG 131A-13 (SHEET1); REPAIR FABRICATED, TREATED, AND PAINTED IAW SRM 53-05 FIG 131A-13 (SHEET 1), SRM 51-10-3 PAR 21 AND 14; REWORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 21 AND 14; THE REPAIR WAS INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 986-991) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LT CUSP WEB FROM BS 986 TO 991 BTW X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-9 SRM 51-10-3 PAR 14 & 21, SRM 51-30-2, AND 51-30-5.

Part: STRUCTURE — CORRODED (BS 649) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LT PREVIOUS DOUBLER X=54 TO 60 BS 649. DOUBLER WAS FABRICATED. REPAIR PARTS WERE TREATED AND PAINTED. REPAIR WERE INSTALLED. CIC WERE APLIED IAW SRM 51-30-2, 53-05, 51-10-3, AND 51-10-3 PAR 38, SRM 53-05 FIG 131A-14, 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 503-522) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LOWER SURFACE OF CUSP WEB X 53 TO 60 FROM BS 503 TO 522. REPAIRED IAW SRM 53-05 FIG 131A.

Part: SEAT TRACK — CORRODED (BS 216-224) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LH SEAT TRACK BS 216 TO 224 AND X 22. THE SEAT TRACK WAS REPLACED IAW SRM 53-05 FIG 4H AND SRM 51-30-1, 51-30-5.

Part: SEAT TRACK — CORRODED (BS 200-224) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON THE LT SEAT TRACK X 44 BS 200-224. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-3 PAR 14, 21, & 26, SRM 51-30-1, SRM 51-10-4, AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 390-395) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB X 57 TO X 60 BS 390 - 395. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-14.

Part: CUSP WEB — CORRODED (BS 724-727) · corrosion level 2 · airframe 66,343 hrs · 49,060 cycles

CORROSION ON LEFT CUSP WEB X 60-54, BS 724 AND 727. THE CUSP WEB WAS REPAIRED AND TREATED IAW SRM 51-30-2, SRM 51-30-5, SRM 53-05 FIG. 131A-10 AND 131A-2, SRM 51-10-3 PAR. 14, 21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON RT CUSP WEB STA Y=856 AND BTW STA Y=890 TO Y=893 BTW X=-54 AND X=-60 AT PAX CABIN STRUCTURE. CUSP WEB RT STA Y=856 AND Y=890 TO 893 WERE REPAIRED IAW SRM 53-05 FIG 131A-13.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON COUNTERSINK AREA ON FUEL ACCESS PLATE 2301 AT CENTER FUEL TANK. CORROSION ON COUNTERSINK AREA ON FUEL ACCESS PLATE 2301C WAS REMOVED AND COUNTERSINK WAS MEASURED THE MAX DIAMETER ALLOWED IS 0.660" AND 7 HOLES WERE FOUND WITH 0.669, 0.672, 0.674, 0.671, 0.706, 0.670, AND 0.695 THEREFORE IS OUT LIMITS AND ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB STA X=54 TO 60 BTW STA Y=618 TO 635 AT PAX CABIN FLOOR STRUCTURE. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05 FIG 131A-14 TREAT AND PAINT IAW SRM 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON RT CUSP WEB BTW X=-54 AND X=-60 STA Y=906 TO Y=911 AT PAX CABIN FLOOR STRUCTURE. DAMAGES WERE REMOVED, NEW PARTS REPAIR WERE FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05 FIG 131A-1 51-10-3 PAR 21, 14, 51-30-2.

Part: CUSP WEB — CORRODED (BS 543-547) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON LT CUSP WEB X 58 TO 60 BS 543 - 547. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PANEL 1460C ON RT WING. CORROSION WAS REMOVED IAW SRM 51-22-2A. THE ACCESS PANE WAS FOUND OUT OF LIMITS AND REPLACED.

Part: CUSP WEB — CORRODED (BS 936) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON RT CUSP WEB BS 936, X -54 AND X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-4 51-10-3 PAR 14 AND 21, 51-30-2.

Part: CUSP WEB — CORRODED (BS 438-443) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON RT CUSP WEB BS 438 - 443, X -60. CORROSION REMOVED. A REPAIR WAS FABRICATED,TREATED, AND PAINTED. THE REPAIR WAS INSTALLED IAW SRM 53-05 FIG 131A-13, SRM 51-10-3 PAR 14 AND 21, SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 458-463) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON THE LT CUSP WEB X 59 BS 458 - 463. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-14 SH-5.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW SRM 51-10-2, DWG 9957858, SRM 51-10-3 PAR 14, 21, & 38 AND SRM 51-30-2.

Part: FINGER DOUBLER — CORRODED (BS 370-389) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON INTERNAL SKIN FINGER DOUBLER REPAIR BTW BS 370 - 389 AND LONGERON 29L. THE FINGER DOUBLER WAS REPLACED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PANEL 1355C, ON LT WING. THE ACCESS PANEL WAS FOUND TO BE OUT OF LIMITS. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 1008-1019) · corrosion level 2 · airframe 66,338 hrs · 49,054 cycles

CORROSION ON RT CUSP WEB BS 1008 TO 1019, X 54 TO X 60. CORROSION WAS REMOVED IAW SRM 53-05 FIG 131A-13, 51-10-3 PAR 21 AND 14

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,823 hrs · 46,490 cycles

CRACKED PAN ON AFTER CUTOUT AT UPPER BEAM AREA OF LT AFT EMERGENCY DOOR. PAN WAS REPAIRED IAW SRM 52-05D, FIG 51, 51-30-1, 51-30-2, 51-30-5, 51-10-2, 51-10-4 AND 51-10-3, PARA 14 AND 21. LP 1927249.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,397 hrs · 49,097 cycles

CORROSION ON RT SEAT TRACK STA Y= 228-230 X=-44. DAMAGE WAS REMOVED, NEW PLUG AND CHANNEL WERE ADJUSTED, TRIMMED AREA OF TRACK WAS TREATED AND PAINTED, NEW PLUG AND CHANNEL WERE INSTALLED.

Part: PAN — CRACKED (BS 984-1003) · airframe 62,823 hrs · 46,490 cycles

CRACK ON RT WINDOW RING PAN BETWEEN BS 984 AND 1003 AT PAX CABIN STRUCTURE FWD LWR CORNER. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA, REV ORIGINAL. LP 1923133.

Part: STRUCTURE — UNKNOWN (VERTICAL STAB) · airframe 49,992 hrs · 37,518 cycles

VERTICAL STAB FRONT SPAR AND SKINS REPAIRED IAW AA 5530-01045.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,454 hrs · 45,532 cycles

DURING CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 1 AND 3. MAINTENANCE REPLACED THE BATTERY PACK AND OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,454 hrs · 45,532 cycles

DURING CHECK, MAINTENANCE FOUND THREE EMERGENCY LIGHTS INOPERATIVE FOR THE TAILCONE SLIDE. MAINTENANCE REPLACED THE LAMPS AND OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 60,600 hrs · 44,896 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE AT SEAT 34D. MAINTENANCE REPLACED THE WIRE HARNESS AND THE LIGHTS RETURNED TO AN OPERATIVE STATE.

Part: SPAR — UNKNOWN (RT WING) · airframe 59,105 hrs · 43,884 cycles

RIGHT WING, REAR SPAR, LOWER CHORD, STA 57, REPAIRED IAW ERA 519928-14.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 59,099 hrs · 43,878 cycles

DURING LINE CHECK, THE AFT EMERGENCY AISLE LIGHTS INOPERATIVE. REPLACED FUSE IN BATTERY PACK AND OPS CHECKED GOOD IAW AMM 33-53.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 59,087 hrs · 43,870 cycles

LEFT INTERNAL SKATE ANGLE, BS 1418 INSIDE ACCESS PANEL 6301B CRACKED. VERTICAL STAB REPAIRED IAW SRM 51-01 AND DWG 5912188.

Part: ANGLE — DAMAGED (VERTICAL STAB) · airframe 59,087 hrs · 43,870 cycles

RT LWR CORNER AND HOLE FOR ATTACH ANGLE ELONGATED. INSTALLED NEW ANGLE AND FRAME IAW DWG 5910242 AND SRM 51-30.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 59,087 hrs · 43,870 cycles

RIGHT INTERNAL SKATE ANGLE, BS 1418, INSIDE ACCESS PANEL, 6301B CRACKED. VERTICAL STAB REPAIRED IAW DWG 5912188 AND SRM 51-01.

Part: DOOR — UNKNOWN (CARGO) · airframe 59,087 hrs · 43,870 cycles

FWD, MID, AFT CARGO DOORS REPAIRED IAW AA 5230-01159.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,888 hrs · 43,712 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING DOORS WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1497) · airframe 58,250 hrs · 43,263 cycles

A CRACK WAS FOUND AT LT SIDE TO FRAME AT BS 1497. REPAIR ACCOMPLISHED IAW ER/A 516104-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,867 hrs · 42,968 cycles

DURING LINE CHECK, MX FOUND THAT THE RED EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPS CONDITION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,846 hrs · 42,247 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 14DE IN THE CABIN WAS INOPERATIVE. MX REPLACED THE SEAT WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: TERMINAL — SEVERED (EMERGENCY LIGHT) · airframe 56,650 hrs · 42,110 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROW 36 WAS INOPERATIVE. MX FOUND THAT A RING TERMINAL ON THE LIGHT RECEPTICAL WAS SEVERED. REPAIR WAS ACCOMPLISHED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 56,718 hrs · 42,162 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 32 IN THE CABIN WAS INOPERATIVE. MX FOUND HIGH RESISTANCE AT THE GROUND CONNECTION AND CLEANED & SECURED. FUNCTIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,718 hrs · 42,162 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CEILING AT ROW 15 IN THE CABIN WAS INOPERATIVE. MX REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,078 hrs · 41,680 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD CABIN EMERGENCY ESCAPE LIGHTING AT ROWS 2 THROUGH 4 AND AT ROW 19 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,981 hrs · 41,611 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY OVERHEAD LIGHTS IN THE COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — UNKNOWN (HORIZONTAL STAB) · airframe 55,697 hrs · 41,392 cycles

HS UPPER CENTER SKIN PANEL REPAIRED AIW AA 5510-01086.

Part: DOOR — BINDING (MID CARGO) · airframe 55,548 hrs · 41,294 cycles

RAMP CREW REPORTED THAT THEY ARE UNABLE TO CLOSE MID CARGO DOOR. WORK ACCOMPLISHED PER ERA 503320-14 REV ORIG REFER TO REVISION O1 FOR STEPS 4-14 OF ERA 503320-14. REPAIR COMPLETED PER ERA 503320-14 REV O.

Part: ATTACH FITTING — CORRODED (NR 2 SLAT) · airframe 55,548 hrs · 41,294 cycles

AT PACKAGE SERVICE VISIT, MAINTENANCE FOUND CORROSION ON THE LEFT NR 2 SLAT INBOUND ATTACH FITTING LUGS. MAINTENANCE COMPLIED WITH THE REPAIR DETAILED IN ERA 475030-14 REV ORIG.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 55,548 hrs · 41,294 cycles

CORROSION ON C3 DOOR SILL BEAM REPAIR BS 1155 - 1212 L28L. REMOVED AND REPLACED CORRODED -9 SPACER AND 6 NUT STRIPS WITH NEW TITANIUM SPACER REF SRM 53-05 AND DWG 5930481.

Part: LUG — UNKNOWN (HORIZONTAL STAB) · airframe 55,539 hrs · 41,289 cycles

HS HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,971 hrs · 40,896 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 32DE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT HARNESS AT SEAT 32DE. OPERATION CHECKS GOOD.

Part: LONGERON — UNKNOWN (UNKNOWN) · airframe 51,423 hrs · 38,503 cycles

NOSE LONGERON REPAIRED IAW EA 09-069225-12.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,556 hrs · 37,889 cycles

MX FOUND THE EMERGENCY LIGHTS LT AND RT OVER THE ROW 2 CEILING PANEL TO BE INOPERATIVE. MX REPLACED THE POWER SUPPLY AT ROW 6C. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,014 hrs · 37,535 cycles

ON LAY OVER FOUND EMERGENCY LIGHT IN SEATS INOP 13-24. FOUND WIRE BROKEN AT SPLICE LOCATION AT SEAT 13 DE. REPAIRED IAW CHAPTER 20.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

LT EXTERNAL FUSELAGE AFT LAV SERVICE DOOR AREA SKIN LWR FWD CORNER HAS EVIDENCE OF CORROSION. REPAIRED SKIN FROM STA 1278-1338 L18L-23L IAW ERA 475018-14 REV ORIG DATED 6/6/09.

Part: SKIN — CORRODED (BS 1278) · airframe 48,378 hrs · 36,464 cycles

AT HMV TEMPORARY REPAIRS OF THE FUSELAGE SKIN WERE BEING REPLACED WITH A SKIN SPLICE FROM STA 1278 TO STA 1338 BETWEEN L-18L AND L-23L WHEN CORROSION WAS FOUND AROUND THE LAV PANEL CUTOUT IN THE SURROUND DOUBLER. THE CORROSION WAS REMOVED AND REPAIRED PER ER/A 475018-14.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 48,378 hrs · 36,464 cycles

C1 DOOR SKIN DOUBLER AT AFT UPPER CORNER OF CUTOUT HAS TEMPORARY FASTENERS INSTALLED. INSTALL PERMANENT REPAIR PER DELTA ERA 462927-14 REV ORG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

CUSP WEB AT STATION 552 LBL 54 CORRODED OUT OF LIMITS. REPAIRED PER DELTA ERA 472914-14 REV ORG.

Part: BRACKET — CORRODED (BS 1497) · airframe 48,378 hrs · 36,464 cycles

RUDDER YAW DAMPER MOUNT BRACKET CORRODED OUT OF LIMITS. REPAIRED BY REPALCEMENT PER 20-30-01 AND 232-13-01.

Part: BRACKET — CORRODED (BS 1497) · airframe 48,378 hrs · 36,464 cycles

RUDDER SECTOR BRACKET CORRODED OUT OF LIMITS AT STATION 1497AT RUDDER TORQUE TUBE. REPAIRED BY REPLACEMENT PER 20-10-17-201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

FORMER STATION 1287 AND LONGERON 24L CORRODED OUT OF LIMITS. REPAIRED PER REPLACEMENT PER 53-03D FIGURE 97.

Part: ROD END — CORRODED (RUDDER PCU) · airframe 48,378 hrs · 36,464 cycles

RUDDER PCU STABILIZATION ROD END CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT PER 20-20-01.

Part: LONGERON — CORRODED (BS 1287 L22L) · airframe 48,378 hrs · 36,464 cycles

LONGERON 22 LEFT CORRODED OUT OF LIMITS AT STATION 1287. REPAIRED BY REPLACEMENT PER 53-02 FIGURE 18.

Part: BRACKET — CORRODED (BS 1497) · airframe 48,378 hrs · 36,464 cycles

RUDDER CABLE PULLEY BRACKET CORRODED OUT OF LIMITS AT STATION 1497 AND LONGERON 3 R. REPAIRED BY REPLACEMENT PER 20-30-01-201.

Part: BRACKET — CORRODED (BS 1431) · airframe 48,378 hrs · 36,464 cycles

RUDDER TRIM CABLE BRACKET CORRODED OUT OF LIMITS AT STATION 1431 LONGERON 4 R. REPAIRED BY REPLACEMENT PER 20-30-01.

Part: SKIN — GOUGED (BS 201 L17R) · airframe 48,378 hrs · 36,464 cycles

GOUGE AT STA 201 AND LONGERON 17R. REPAIRED IAW ERA 473065-14 REV ORG, TRIM OUT, FILLER AND DOUBLER.

Part: SKIN — DENTED (L1 DOOR) · airframe 48,378 hrs · 36,464 cycles

L1 DOOR DENTED AT FWD CORNER. REPLACED SKIN IAW 52-05 FIG 37.

Part: CUSP WEB — CORRODED (BS 465) · airframe 48,378 hrs · 36,464 cycles

LBL 54 CUSP WEB AT STATON 465 TO 522 CORRODED OUT OF LIMITS. REPAIRED PER DELTA ERA 472917-14 REV ORG.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 48,378 hrs · 36,464 cycles

LT INBD FLAP LOWER SURFACE DAMAGED WITH SEVERAL GOUGES. REPLACED SKIN IAW 57-50-14 AND 51-30-02.

Part: BEAM — CORRODED (AFT CARGO CUTOUT) · airframe 48,378 hrs · 36,464 cycles

AFT CARGO DOOR CUTOUT LWR BEAM CORRODED OUT OF LIMITS. REPAIRED IAW 53-04 FIGURE FIGURE 123.

Part: LONGERON — CORRODED (BS 1174 L30L) · airframe 48,378 hrs · 36,464 cycles

LONGERON 30 LT, CORRODED IN AFT CARGO COMPARTMENT STA 1174. REPAIRED IAW ERA 478071-14 REV ORG.

Part: SKIN — DENTED (BS 587-633) · airframe 48,378 hrs · 36,464 cycles

FUSELAGE SKIN STA 587 TO 636 AND LONGERON 23R DENTED ABOVE STATIC PORT. REPLACED FUSELAGE SKIN FROM STA 587 TO 636 FROM LONGERON 23 L TO L 26 L IAW SRM 53-04D FIGURE 12C AND 12E. CLASS 1 REPAIR - 8000 CYCLE, REPEAT VISUAL INSPECTION.

Part: BRACKET — CORRODED (BS 1480) · airframe 48,378 hrs · 36,464 cycles

ELEVATOR BRACKET PULLEY CORRODED AT STA 1480. REPAIRED BY REPLACEMENT.

Part: FRAME — CORRODED (BS 1287 L28L/R) · airframe 48,378 hrs · 36,464 cycles

AFT CARGO FRAME STA 1287 LONG 28R TO 28L CORRODED. REPAIRED IAW SRM 53-14-3, 51-30-2,

Part: FRAME — CORRODED (BS 1250 L27R) · airframe 48,378 hrs · 36,464 cycles

AFT CARGO CIRCUMFERENTAL FRAME AT STA 1250 LONG 27R CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMIT. REPAIRED IAW SRM 53-03D FIG 2A AND 53-01, FIG 1.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 48,378 hrs · 36,464 cycles

LT INBD FLAP, INBD VANE HAS DENTS AND PUNCTURE ON EXISTING REPAIR LWR SURFACE. REPAIRED IAW ERA 4731169-14 REV ORIG. DATED 5/20/09.

Part: TAB — DENTED (LEFT ELEVATOR) · airframe 48,378 hrs · 36,464 cycles

LT ELEVATOR ANTI FLOAT TAB LWR SURFACE DENTED OUT OF LIMITS 10 INCHES FROM INBD END. REPAIRED IAW 51-70-2 PAGE 59 ON AAR 264670.

Part: CUSP WEB — CORRODED (BS 809) · airframe 48,378 hrs · 36,464 cycles

RT CUSP WEB F/S 809 HAS CORROSION AROUND LIGHTENING HOLE. REPAIRED IAW SRM 53-05.

Part: TAB — DAMAGED (LEFT AILERON) · airframe 48,378 hrs · 36,464 cycles

LT AILERON CONTROL TAB T/E DAMAGED 6 INCHES FROM INBD END. REPAIRED IAW SRM 51-90-0 PARA 8N PG 72.

Part: VANE — PUNCTURED (LT WING TE FLAP) · airframe 48,378 hrs · 36,464 cycles

LT INBD FLAP OTBD VANE HAS PUNCTURES AND GOUGES LWR INBD SIDE. REPAIRED LT INBD FLAP OTBD VANE LWR SURFACE DAMAGE IAW SRM 57-03D FIG 11.

Part: BRACKET — CRACKED (HORIZONTAL STAB) · airframe 48,378 hrs · 36,464 cycles

LT ANTI FLOAT TAB IB SECTOR BRACKET HAS A BROKEN GUIDE PIN EAR. REPAIRED BY REPLACEMENT IAW 27-30.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

RUDDER CABLE BELOW YAW DAMPNER CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT IAW 27-20.

Part: INTERCOSTAL — CORRODED (BS 1212) · airframe 48,378 hrs · 36,464 cycles

AFT CARGO INTERCOSTAL STA 1212 LONGERON 29L CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT IAW 51-30-2 FIG 2 AND 51-30-5 PAGE 13.

Part: SEAT TRACK — CORRODED (BS 1205) · airframe 48,378 hrs · 36,464 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS AT STATION 1205 AND LBL 44. REPAIRED IAW 53-05 FIGURE 4 SEAT TRACK SPLICE REPAIR.

Part: FRAME — CRACKED (BS 1174 L5L) · airframe 48,378 hrs · 36,464 cycles

FRAME 1174 CRACKED AT LONGERON 5L. REPAIRED IAW 53-03D FIGURE 4.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1350) · airframe 48,378 hrs · 36,464 cycles

FLOOR SUPPORT AT RBL 18 AND STA 1309-1350 CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT IAW 51-10-4 AMD 51-10-30.

Part: BRACKET — CORRODED (BS 1497) · airframe 48,378 hrs · 36,464 cycles

MAIN RUDDER SECTOR BRACKET CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT IAW 27-20.

Part: SEAT TRACK — CORRODED (BS 498) · airframe 48,378 hrs · 36,464 cycles

SEAT TRACK STA 498, RBL 54 CORRODED OUT OF LIMITS. REPAIRED IAW 53-05D FIGURE 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

INSTERCOSTAL CRACKED ATO AIRSTAIR DOOR CUT OUT. REPAIRED BY REPLACEMENT PER 51-30-1 AND DWG 9910078.

Part: CUSP WEB — CORRODED (BS 503-598) · airframe 48,378 hrs · 36,464 cycles

RT CUSP WEB STA 503 TO 598 CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT IAW 51-30-02 ON AAR NR 246207.

Part: CUSP WEB — CORRODED (BS 703) · airframe 48,378 hrs · 36,464 cycles

RT CUSP WEB STATION 703 HAS CORROSION AT RBL 54. INSTALLED DOUBLER IAW 53-01 FIGURE 4 SHEET 4.

Part: ANGLE — CORRODED (BS 1401) · airframe 48,378 hrs · 36,464 cycles

ANGLE CORRODED, STA 1401, LBL 20 LONGERON. REPAIRED BY REPLACEMENT IAW 51-30-5 /2 AND 5911429.

Part: SUPPORT ANGLE — CRACKED (BS 1463 L6L) · airframe 48,378 hrs · 36,464 cycles

CANTED FRAME SUPPORT CRACKED AT STA 1443 LT LONGERON 6 . REPAIRED BY REPACEMENT IAW 51-3-5 AND DWG 5930556.

Part: FLOORBEAM — CORRODED (BS 155) · airframe 48,378 hrs · 36,464 cycles

FLOOR SUPPORT AT STATION 155 RBL 50 CORRODED OUT OF LIMITS. REPAIRED REPLACEMENT PER 53-10 AND 51-10-04 ON NR 246891.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,378 hrs · 36,464 cycles

SCRATCH IN RT SIDE FUSELAGE AFT AND ABOVE POTABLE WATER SVC PANEL. REPAIRED IAW DWG SG09530001.

Part: WEB — CORRODED (BS 560-598) · airframe 48,378 hrs · 36,464 cycles

LT CUSP WEB FS 560-598 HAS AREAS OF CORROSION. REPAIRED CUSP WEB 2 EACH IAW SRM 53-05D.

Part: CUSP WEB — CORRODED (BS 826) · airframe 48,378 hrs · 36,464 cycles

CUSP WEB AT STATION 826 LBL54 CORRODED OUT OF LIMITS. REPAIRED PER 53-05 FIGURE 827D PG 884-886.

Part: ANGLE — CORRODED (BS 1118-1136) · airframe 48,378 hrs · 36,464 cycles

FLOOR ANGLE STA 1118 TO 1136 AT LBL 56 CORRODED. REPAIRED BY REPLACEMENT PER 53-10-03 ON AAR 246188.

Part: CUSP WEB — CORRODED (BS 1041) · airframe 48,378 hrs · 36,464 cycles

RT CUSP WEB RBL 54 AT STATION 1041-1079 CORRODED OUT OF LIMITS. REPAIRED PER DELTA ERA 398191-14MA REV A. CORROSION WAS LEVEL 2 CORROSION.

Part: CUSP WEB — CORRODED (BS 712-788) · airframe 48,378 hrs · 36,464 cycles

CUSP WEB AT RBL 54 AND STATION 712-788 CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT PER 53-04 FIG 827D SHEET 1-4.

Part: LONGERON — CRACKED (BS 200 L23L) · airframe 48,378 hrs · 36,464 cycles

FOUND LONGERON 23L CRACKED AT UPPER LOCK FASTENER ATTACHMENT TO FS 200 FRAME. REPAIRED CRACKED LONGERON IAW SRM 53-02 FIG 18.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 48,153 hrs · 36,321 cycles

FWD GALLEY 1R DOOR SLIDE DEPLOYED. REPLACED 1R DOOR SLIDE PER OPN 7035, S/N OFF - 1891, S/N ON - 0344.

Part: SKIN — DAMAGED (BS 427-465) · airframe 44,520 hrs · 33,951 cycles

THE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, C1 DOOR CUTOUT SURROUND DOUBLER, LONGERON, AND FRAME AFT OF THE FWD CARGO DOOR CUTOUT BETWEEN STA 427 - STA 465 AND L-19R- L20R. SPLICED A NEW SECTION OF FUSELAGE SKIN BETWEEN STA 394 AND STA 494, FROM L-18R TO L-26R. THE FRAME AND LONGERON REPAIR WAS ACCOMPLISHED PER SRM. AN EXTERNAL REPAIR WAS INSTALLED AT THE UPPER AFT CORNER OF THE C1 DOOR CUTOUT TO REPAIR THE SURROUND DOUBLER.

Part: SKIN — PUNCTURED (FS 218 L18R) · airframe 43,332 hrs · 33,165 cycles

FUSELAGE SKIN PUNCTURED FROM CONTACT WITH GSE EQUIPMENT. DAMAGE LOCATED AT FS 218, ABV L-18R. CUT OUT DAMAGE AND INSTALL MODIFIED REPAIR PER MD-88 SRM 53-04 FIG 12B CLASS III REPAIR.

Part: SKIN — GOUGED (FS 1155) · airframe 41,198 hrs · 31,693 cycles

THE FUSELAGE SKIN WAS FOUND DAMAGED AT THE EDGE OF THE PANEL AT THE AFT CARGO DOOR OPENING AT FS 1155. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: GENERATOR — DAMAGED (LT ENGINE) · airframe 34,018 hrs · 26,598 cycles

A C LOCKOUT WITH LT GEN INOP MESSAGE IN FLIGHT - FOUND GENERATOR WINDINGS COMING APART - REPLACED LT CSD AND GEN.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 33,284 hrs · 26,091 cycles

DURING ACCOMPLISHMENT OF EA09-075135-03AD, MEO1 OPN 0101 GRAPHIC 1, SHEET 3 STEP 1, THE P-DOME LOWER T-ANGLE WAS DAMAGED. THERE IS NO DAMAGE ALLOWED IN THIS AREA {REF SRM 53-05D FIG 115}. THE ONLY FIX IS TO SPLICE A IN A NEW SECTION {REF SRM 53-03D FIG 37}. THERE IS A CONCERN THAT SINCE THIS EA HAS BEEN ACCOMPLISHED ON ALL A/C, THERE ARE OTHER A/C IN SERVICE, POSSIBLY FOR LONG PERIODS OF TIME, WITH THIS SAME CONDITION.

Part: PSEU — MALFUNCTIONED (E & E BAY) · airframe 32,596 hrs · 25,606 cycles

ON LANDING GEAR EXTENSION, DID NOT RECEIVE A GREEN OR RED GEAR POSITION LIGHT. VISUALLY CHECKED (TOWER & PERISCOPE ) LANDING GEAR FOR SAFE INDICATIONS. ON POWER TRANSFER TO GROUND POWER, GEAR POSITION LIGHTS BECAME GREEN & CYCLED, UNSAFE TWICE ( RED LIGHTS WITH CAWS WARNING). PERFORMED BITE ON PROX BOX. DURING BITE GEAR INDICATION RETURNED TO NORMAL. GREEN LIGHTS ON. R & R PROX BOX PER MM 32-60-04-02 CHECKS. GOOD.

Part: LINK — LOOSE (LEFT) · airframe 30,695 hrs · 24,206 cycles

ON APPROACH AILERONS JAMMED -REPLACED THE LEFT AILERON I/B CRANK ASSY FOR EXCESSIVE PLAY

Part: PANEL — DELAMINATED (LEFT UPPER) · airframe 29,002 hrs · 22,880 cycles

LT. OVER WING ACCESS PANEL DELAMINATED AND TORN - REPLACED SAME

Part: LINE — LEAKING (HYD SYSTEM) · airframe 28,485 hrs · 22,503 cycles

BAD ODOR IN CABIN DURING TAKEOFF AND LANDING. FOUND HYDRAULIC LINE LEAKING ON LEFT THRUST REVERSER CONTROL VALVE. TIGHTENED LINE. PERFORMED OPN 5088 DUCT BURNOUT

Part: CHARGER — ODOR (E/E BAY) · airframe 26,046 hrs · 20,710 cycles

DURING EMERGENCY POWER CHECK, BATTERY CHARGER GAVE OFF A STRONG BURNING ELECTRICAL SMELL. REPLACED BATTERY CHARGER PER MAINTENANCE MANUAL.

Part: WIRE — BROKEN (ROW 24 - 30)

EMERGENCY LIGHTS INOP BETWEEN ROWS 24-30. REPAIRED WIRES BROKEN AT WALL SPLICE AND REPLACED BAD PWR SUPPLY LIGHTS, NOW CK GOOD.

Part: AIR DISTRIBUTION — SMOKE (CABIN)

APPROX ONE TO TWO MINUTES AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. BOTH SMOKE DETECTORS IN REAR OF AIRCRAFT ACTIVATED. CHECKED APU INLET FOUND CLEAR. PERFORMED DUCT BURNOUT PER M/M 36-10-00-5. NO SMOKE IN CABIN ON RUN-UP. OK FOR SERVICE.

Part: HYD LINE — LEAKING (TAIL COMPT)

SMELLED SMOKE IN CABIN WHEN APU STARTED ON APPROACH. FOUND LEAKING HYDRAULIC LINE IN TAIL COMPARTMENT. REPAIRED, PERFORMED DUCT BURN-OUT.

Part: COFFEEMAKER — FAILED (GALLEY)

THE FORWARD GALLEY COFFEEMAKER CIRCUIT BREAKER POPPED, THE F/A NOTICED A BURNING SMELL AND HEARD A POPPING NOISE, NOTICED THE C/B THEN POPPED. CONTACTED ATL MCC. REPLACED F/C COFFEEMAKER, RESET C/B, BREWED COFFEE. OPS NORMAL, NO SMELL NOTED.

Part: FRAME — CORROSION (BS 1307)

THE FUSELAGE STAION 1307 LOWER FRAME WAS FOUND WITH SEVERE CORROSION BETWEEN STRINGERS 29L AND 29R. DUE TO THE EXTENT OF THE CORROSION, A REPLACEMENT SECTION WILL BE SPLICED IN. THE FRAME WILL BE CUT AT STRINGER 29L AND 29R. REPAIRED PER ERA 330754-14 REV B.

Part: SKIN — CORROSION (BS 772/806)

CORROSION WAS FOUND UNDER THE RIGHT RUB STRIP AT FS 772 AND 806 BETWEEN STR 27R AND 29R. THE RUB STRIP IS LOCATED WHERE THE WING TO BODY FAIRING MEETS THE FUSELAGE. THE BLEND DEPTH AND LOCATION FOR THE DAMAGE NOT CONSIDERED ALLOWABLE PER THE SRM IS LOCATED IN TABLE 1. THE SKIN WAS CUTOUT AT STATION 772 TO A DIAMETER OF 1.125. THE LOCAL THICKNESS AT THE CUTOUT IS .092 THE SKIN IS M/F FROM .160 7075-T6 CLAD SHEET AT FS 817 AND TAPERS DOWN TO .080 AT FS 759. THE LOCAL SKIN THICKNESS AT THE AFT DAMAGE LOCATION IS .160. REPAIRED PER ERA 330741-14 REV A.

Part: FRAME — CRACKED (BS 1418)

AT FS 1418, MTC FOUND A .625 CRACK ON L-2L AND A .75 CRACK ON L-2R, AT THE TYPICAL LOCATIONS COVERED BY EO 9-63538-03. THE A/C COVERED IN THIS ER/A IS NOT COVERED BY THE REFERENCE EO (A/C NR 901-963), BUT AS A REPAIR AND PREVENTION OF FUTURE FATIGUE, THE EO WILL BE PERFORMED ON THIS A/C.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

GEAR WOULD NOT RETRACT AFTER T/O. HANDLE WOULD NOT MOVE FROM THE HALFWAY POSITION. RED EAR WARNING LIGHTS REMAINED ILLUMINATED AND HANDLE WAS FROZEN UNTIL THE ALT GEAR EXT LEVER WAS CYCLED. CKD GEAR HANDLE AND LINKAGE, CYCLED GEAR SEVERAL TIMES. CKD LINKAGE AND CABLES, CYCLED AGAIN. ALT GEAR EXTENSION, CYCLED. CKD NOSE GEAR STRUT EXTENSION, ALL INDS NORM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

FOUND ON LAYOVER 2 CHECK F/C AND REAR TOURIST CLASS EMERGENCY TRACK LIGHTING INOP. REINSTALLED REAR BATTERY PACK AND REPLACED F/C POWER SUPPLY (S/N 1275) ON, (S/N 8091) OFF, (P/N 337701962).

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE)

AFTER ATTAINING T/O PWR, NR 1 ENGINE ROLLED BACK, PRESSURIZATION WAS LOST. NR 1 ENGINE DID COME BACK WITH NORMAL OPS DURING CLIMB. MX IN PROGRESS REPLACING FUEL PUMP AND FUEL CONTROL.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLASHLIGHT FWD F/A LOW BATTERY. REPLACED BATTERY, OPS CKS NORMAL.

Part: DUCT — CRACKED (NR 2 ENGINE)

ABE - AFTER T/O, THE NR 2 FIRE WARNING SOUNDED, WOULD STOP WITH THROTTLES PLACED AT IDLE. MTC FOUND THE 13TH STAGE COWL ANTI-ICE VALVE DUCT BLOWN ON THE ENG SIDE OF THE VALVE. REPLACED DUCT, OPERATION NORMAL.

Part: ANGLE — CRACKED (RT MLG WW)

FOUND DURING E-1 LETTER CHECK, 1.5 INCH CRACK IN STRIKER ANGLE AFT O/B SIDE OF RT WHEEL WELL. REPAIRED PER SRM 53-05.

Part: NOSE COWL — DENTED (NR 1 ENG)

1 INCH BY 1 INCH DENT IN NOSE COWL AT 1200 POS. REPAIRED INSP PER SRM 54-04 FIG 9. FOUND AT LETTER CHECK.